FIELD OF THE INVENTION
[0001] The present invention relates to a method of producing sintered - or bond- rare earth
element·iron·boron magnets superior in magnetic properties.
DESCRIPTION OF THE PRIOR ART
[0002] Rare earth element·iron·born permanent magnets are highly praised for the superior
magnetic properties. Japanese Patent Publication B-61-34242 discloses a magnetically
anisotropic sintered permanent magnet composed of Fe-B-R (R: rare earth element).
For the production, an alloy containing the above-mentioned components is cast, the
cast alloy is pulverized to an alloy powder, and the alloy powder is molded and sintered.
However, the pulverization of cast alloy is a costly step, and the performance of
product fluctuates between production batches. Japanese Patent Publication B-3-72124
discloses a production method of an alloy powder for rare earth element·iron·born
permanent magnets containing as the main component 8-30 atomic% of R (R is at least
one rare earth element including Y), 2-28 atomic% of B and 65-82 atomic% of Fe. The
production method comprises steps of reducing the raw material powder composed of
a powder of rare earth oxide and a powder of metal and/or alloy with a metallic Ca
or CaH₂ reducing agent, heating the reduced material in an inert atmosphere, and removing
byproducts by leaching with water. Problems accompanied by the method are that steps
of removing byproducts and drying are required due to employment of the metallic Ca
or CaH₂ reducing agent, the alloy powder is readily oxidized by air as the powder
is so fine as 1-10 µm, and the oxygen-containing powder brings about inferior magnetic
properties in the final product. So, careful handling of the powder product is requested
and it necessitates equipments/steps for measuring, mixing and molding thereof under
air-insulated conditions, which cause an increase in the production cost.
SUMMARY OF THE INVENTION
[0003] It is an object of the present invention to provide a method of producing sintered-
or bond- rare earth element·iron·boron magnets obtainable easily and superior in magnetic
properties with stable performance.
BRIEF DESCRIPTION OF THE DRAWINGS
[0004] Fig.1 is a flow chart showing preparation of a sintered magnet and a bond magnet
in which aluminum phosphate is used as a heat resistant coating material.
[0005] Fig.2 is a flow chart showing preparation of a sintered magnet and a bond magnet
in which a poorly heat-resistant silicone oil or a film forming synthetic resin is
used as the coating material.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0006] The method of producing sintered rare earth element·iron·boron magnets according
to the present invention is characterized by that it comprises steps of mixing in
a scheduled ratio an acicular iron powder coated with a coating material, a rare earth
element powder coated with a coating material and a boron powder coated with a coating
material, and subjecting the mixture to compression molding followed by sintering
of the molded mixture in the presence of a magnetic field.
[0007] The method of producing bond rare earth element·iron· boron magnets according to
the present invention is characterized by that it comprises steps of mixing in a scheduled
ratio an acicular iron powder coated with a coating material, a rare earth element
powder coated with a coating material and a boron powder coated with a coating material,
preparing from the mixture a sintered magnet by compression-molding and sintering
in the presence of a magnetic field, preparing a magnet powder by hydrogen-disintegration
of the magnet wherein a hydrogen-occluded magnet resulted from heating the magnet
under hydrogen atmosphere is subjected to hydrogen emission under substantial vacuum
to cause disintegration of the hydrogen-occluded magnet, coating the magnet powder
with a coating material, mixing the coated magnet powder with a binder, and compression
molding the mixture under heating and in the presence of a magnetic field.
[0008] A preferable acicular iron powder is obtained by reducing acicular FeOOH (geothite)
crystal under hydrogen atmosphere at 300-500°C, and the length is not longer than
10µm as exemplified by 1.0µm in length and 0.1µm in width. The acicular iron powder
is employed for the present invention in a state of being coated with a coating material,
and such a heat resistant coating material as aluminum phosphate can coat the acicular
iron powder conveniently by reducing a mixture of acicular FeOOH and aluminum phosphate
under hydrogen atmosphere to bring about an acicular iron powder coated with aluminum
phosphate in a kiln. When such poorly heat resistant coating materials as film-forming
synthetic resins like silicone oils and polyvinyl butyral are employed, they are mixed
in a state of solution with an acicular iron powder prepared by the reduction of FeOOH,
and a coated acicular iron powder is obtained upon drying of the mixture. Since the
acicular iron powder taken out of the kiln should not get in touch with air prior
to being coated, care must be taken for the equipment and handling. Therefore, heat
resistant coating materials like aluminum phosphate are specifically preferred.
[0009] As for the rare earth element, such rare earth elements generally used for rare earth
element·iron·boron permanent magnets as Nd, Pr, Dy, Ho, Tb, La, Ce, Pm, Sm, Eu, Gd,
Er, Tm, Yb, Lu, and Y are mentioned, and one or more than two kinds thereof are employed.
Among them, neodymium (Nd) is used preferably. The rare earth element can be employed
as alone or as a mixture. In the present invention, selections and mixing ratios of
the rare earth element are determined appropriately in accordance with formulations
disclosed in the prior art. The rare earth element is preferably pulverized to have
an average particle size of around 1-10µm in order that the particle can diffuse readily
during the sintering step. The rare earth element may be pulverized mechanically,
however, for the purpose of preventing oxygen effects, it is preferred to adopt a
hydrogen-disintegration method in which hydrogen-occluded rare earth element lumps
resulted from heating rare earth element lumps under hydrogen atmosphere are subjected
to hydrogen emission under substantial vacuum to cause disintegration of the hydrogen-occluded
rare earth element lumps. The hydrogen-occluded rare earth element lumps are prepared
by heating the lumps at 800-900°C under hydrogen atmosphere, and the emission of hydrogen
under substantial vacuum is carried out preferably at a temperature not lower than
100°C. If necessary, the hydrogen-disintegration method can be repeated, and rare
earth element powder of an average particle size of 1-10µm can be obtained, and hydrogen
occlusion for previously disintegrated lumps can be conducted at a lower temperature
like 500°C, as already disintegrated lumps can occlude hydrogen readily. In the present
invention, the pulverized rare earth element powder is employed in a state of being
coated with a coating material, and such a heat resistant coating material like aluminum
phosphate can coat a pulverized rare earth element in a rotary kiln by carrying out
the hydrogen-disintegration method for rare earth element lumps added with aluminum
phosphate. When such poorly heat resistant coating materials as film-forming synthetic
resins like silicone oils or polyvinyl butyral are employed, they are mixed in a state
of solution with a rare earth element powder, and a coated rare earth element powder
is obtained upon drying of the mixture. Since a rare earth element powder taken out
of a kiln should not get in touch with air prior to being coated, care must be taken
for the equipment and handling. Therefore, heat resistant coating materials like aluminum
phosphate are specifically preferred.
[0010] In the present invention, a boron powder employable has preferably an average particle
size of 1-10µm. The boron powder is available similarly to pulverized rare earth elements
by the hydrogen-disintegration method. In this case, it is preferred that hydrogen
is occluded by boron lumps under hydrogen atmosphere at 800-900°, and the occluded
hydrogen is emitted under substantial vacuum at a temperature not lower than 100°C.
If necessary, the hydrogen-disintegration method can be repeated, and boron powder
of an average particle size of 1-10µm can be obtained, and hydrogen occlusion for
previously disintegrated lumps can be conducted at a lower temperature like 500°C,
as already disintegrated lumps can occlude hydrogen readily. For the coating material,
such heat-resistant materials as aluminum phosphate are preferred due to reasons similar
to those for the rare earth elements.
[0011] As for the coating material, heat resistant materials like aluminum phosphate are
especially preferred, as mentioned previously. Aluminum phosphate is available in
a powder form, however, it may be used in a form of solution like an ethanolic solution
for intimate and uniform adhesion to raw materials for magnet. For the adherence of
aluminum phosphate to raw materials for magnet, it can be conducted, for example,
by simply adding a 10% ethanolic solution of aluminum phosphate to the raw materials
for magnet. Aluminum phosphate remained in the final product affects the magnetic
properties not unfavorably but improvably in combination with the oxidation preventing
effect. Further, the coating material to be applied on raw materials for magnet may
include solutions of such film-forming organic materials as synthetic resins like
silicone oils and polyvinylbutyral. Since they decompose at temperatures employed
for reduction by hydrogen of FeOOH (300-500°C) or those for occlusion of hydrogen
by rare earth elements or boron (800-900°C), these organic coating materials must
be applied to raw materials for magnet already encountered with the heat treatment.
This means that though they are applicable to such raw materials as an acicular iron
powder and powder of a rare earth element or boron, since these raw materials are
readily oxidized by air, precautions for handling and equipments are required and
troublesome processing are necessary by comparison with the case of employing aluminum
phosphate capable of being applied prior to the heat treatment. The weight ratio of
the coating material to a rare earth element powder, a boron powder or an acicular
iron powder is 8:1 - 20:1 respectively.
[0012] Thus obtained acicular iron powder coated with a coating material, rare earth element
powder coated with a coating material and boron powder coated with a coating material
are mixed in a scheduled ratio, and the mixture is compression-molded in the presence
of a magnetic field and the molded mixture is sintered in the presence of a magnetic
field to obtain a sintered rare earth element·iron·boron magnet.
[0013] The mixing ratio of raw materials for magnet is settled arbitrary in accordance with
formulations disclosed in the prior art, and the ratio of 20-40 weight% for an rare
earth element powder, 0.5-3 weight% for a boron powder and the rest is for the acicular
iron powder is appropriate. Other than these raw material components, powders of molybdenum,
niobium, etc. may be added for improving temperature characteristics of the magnet,
and the powders are preferably coated with a coating material.
[0014] The magnetic force, compressing pressure, temperatures or period of time for the
sintering step may be determined in accordance with conditions disclosed in the prior
art. Sintered rare earth element·iron·boron magnets are obtained usually by sintering
under an inert gas atmosphere at 1000-1200°C for 1-2 hours. During sintering of materials
for magnet mixed in a scheduled ratio, the rare earth element and boron disperse into
the acicular iron powder oriented perpendicular to the magnetic field to form an alloy
having a specified composition, and a permanent magnet is obtained.
[0015] The raw material for the bond magnet is prepared by disintegration of the above-obtained
sintered magnet. Since mechanical disintegration may destroy an acicular iron crystal,
a hydrogen-disintegration method is employed. According to the hydrogen-disintegration
method, a hydrogen-occluded rare earth element resulted from heating the sintered
magnet under hydrogen atmosphere is subjected to hydrogen emission under substantial
vacuum to cause disintegration of the sintered magnet. The hydrogen-occlusion of rare
earth element in the sintered magnet is conducted by heating the magnet at 800-900°C
under hydrogen atmosphere, and the emission of hydrogen under substantial vacuum is
carried out preferably at a temperature not lower than 100°C. If necessary, the hydrogen-disintegration
method can be repeated, and magnet powder of an average particle size of 1-10µm can
be obtained, and hydrogen occlusion for previously disintegrated magnets can be conducted
at a lower temperature like 500°C, as already disintegrated magnets can occlude hydrogen
readily. Sintered magnet to be used as raw materials for the bond magnet is preferably
prepared to become softer than a sintered magnet product for the convenience of being
subjected to the hydrogen-disintegration method. Since the pulverized sintered magnet
is readily oxidized by oxygen in air, it is employed in a state of being coated with
a coating material, and such a heat resistant coating material like aluminum phosphate
is preferably used due to the same reason as that for rare earth elements. In case
of employing aluminum phosphate as the coating material, it is possible to obtain
a pulverized sintered magnet coated with aluminum phosphate in a rotary kiln in which
lumps of sintered magnet are mixed with aluminum phosphate, heated at 600-1200°C under
hydrogen atmosphere, and disintegrated by emission of hydrogen occurring under substantial
vacuum. When such poorly heat resistant coating materials as film-forming synthetic
resins like silicone oils or polyvinyl butyral are employed, they are mixed in a state
of solution with a pulverized sintered magnet obtained by the pulverization of lumps
of sintered magnet, and a sintered magnet powder coated with the coating material
is obtained upon drying of the mixture. The weight ratio of a coating material to
the of sintered magnet powder is preferably 8:1 - 20:1.
[0016] Magnetically anisotropic permanent magnets are obtained by mixing the above-mentioned
magnet powder coated with a coating material and a binder, and subjecting the mixture
to compression molding under heating in the presence of a magnetic field. The existence
of magnetic field causes the acicular powder to orient vertically. Conditions for
the compression molding are the same as those for preparation of conventional bond
permanent magnets. The binder includes polymeric materials like epoxy resins, polyamide
resins and vitrification agents like MnO, CuO, Bi₂O₃, PbO, Tl₂O₃, Sb₂O₃, Fe₂O₃ and
mixture thereof. For the preparation of bond magnets, powders of molybdenum, niobium,
etc. may be added together with a binder for improving temperature characteristics
of magnets.
[0017] Fig.1 is a flow chart showing preparation of a sintered magnet and a bond magnet
in which aluminum phosphate is used as a heat resistant coating material. The first
step is for the preparation of an acicular iron powder, in which aluminum phosphate
coated acicular FeOOH is reduced in a rotary kiln at 300-500°C under hydrogen atmosphere
to obtain an acicular iron powder coated with aluminum phosphate (1). The second step
is for the preparation of a rare earth element powder, in which aluminum phosphate
coated lumps of rare earth element is heated in a rotary kiln at 800-900°C under hydrogen
atmosphere to occlude hydrogen, subjecting the hydrogen occluded lumps to substantial
vacuum to cause emission of hydrogen at temperatures lowered to 100-300°C to disintegrate
the lump to obtain a rare earth element powder coated with aluminum phosphate (2).
The disintegration with hydrogen emission is repeated until the powder has a scheduled
particle size. The third step is for the preparation of a boron powder, in which aluminum
phosphate coated lumps of boron is heated in a rotary kiln at 800-900°C under hydrogen
atmosphere to occlude hydrogen, subjecting the hydrogen occluded lumps to substantial
vacuum to cause emission of hydrogen at temperatures lowered to 100-300°C to disintegrated
the lump to obtain a boron powder coated with aluminum phosphate (3). The disintegration
with hydrogen emission is repeated until the powder has a scheduled particle size.
The fourth step is for the preparation of a sintered magnet, in which the above-mentioned
(1), (2) and (3) are mixed in a scheduled ratio, the mixture is compression molded
and then the molded material is sintered in the presence of a magnetic field to obtain
a sintered rare earth element·iron·boron magnet. The fifth and sixth steps are for
the preparation of a bond magnet, in which a sintered magnet obtained similarly to
the sintered magnet is coated with aluminum phosphate, the coated magnet is heated
in a rotary kiln at 800-900°C under hydrogen atmosphere to occlude hydrogen, subjecting
the hydrogen occluded magnet to substantial vacuum to cause emission of hydrogen at
temperatures lowered to 100-300°C to disintegrate the magnet to obtain a magnet powder
having a particle size of 1-10µm. The disintegration with hydrogen emission is repeated
until the powder has a scheduled particle size. A mixture of the magnet powder and
a binder is compression molded under heating in the presence of a magnetic field to
obtain a bond rare earth element·iron·boron magnet.
[0018] Fig.2 is a flow chart showing preparation of a sintered magnet and a bond magnet
in which a poorly heat-resistant silicone oil or a film forming synthetic resin is
used as the coating material. The steps indicated are the same as those of Fig.1 with
the exception that already pulverized raw materials for magnet including an articular
iron powder, a rare earth element powder and a boron powder are coated with the coating
material. Although a heat resistant coating material like aluminum phosphate can be
employed in this case, its heat resistant characteristics cannot be utilized.
[0019] The present invention will be illustrated hereunder by reference to examples, however,
the invention never be restricted by the following Examples.
[Example 1]
[0020] To an acicular FeOOH (geothite; TITAN KOGYO K.K.) crystal was added a 10% ethanol
solution containing aluminum phosphate of an amount corresponding to 5 weight% of
the amount of Fe, and the resulted material was mixed and dried. The dried mixture
was subjected to reduction for 1 hour in a rotary kiln under ventilation of 10 liter/min
of 100 vol% hydrogen gas and at 450°C (heating up or cooling rate was 5°C/min) to
obtain an aluminum phosphate coated acicular iron powder of 0.9µm length and 0.09µm
width. To a neodymium (Nd) ingot (5cmx5cmx5cm, containing about 20% of Pr and Dy)
was added a 10% ethanol solution containing aluminum phosphate of an amount corresponding
to 5 weight% of the ingot, and the ethanol was evaporated. The dried Nd ingot was
subjected to hydrogen occlusion for 1 hour in a rotary kiln under ventilation of 10
liter/min of 100 vol% hydrogen gas and at 880°C (heating up rate was 5°C/min), and
then was subjected to emission of hydrogen in substantial vacuum during maintaining
for 1 hour at the temperature followed by cooling to 200°C (cooling rate was 5°C/min)
to disintegrate the Nd ingot. Three times repetition of the disintegration step resulted
in an aluminum phosphate coated Nd powder having an average particle size of 8µm.
To a boron (B) ingot (5cmx5cmx5cm) was added a 10% ethanol solution containing aluminum
phosphate of an amount corresponding to 5 weight% of the ingot, and the ethanol was
evaporated. The dried B ingot was subjected to hydrogen occlusion for 1 hour in a
rotary kiln under ventilation of 10 liter/min of 100 vol% hydrogen gas and at 880°C
(heating up rate was 5°C/min), and then was subjected to emission of hydrogen in substantial
vacuum during maintaining for 1 hour at the temperature followed by cooling to 200°C
(cooling rate was 5°C/min) to disintegrate the B ingot. Three times repetition of
the disintegration step resulted in an aluminum phosphate coated B powder having an
average particle size of 8µm. Thus obtained aluminum phosphate coated Nd powder, aluminum
phosphate coated B powder and aluminum phosphate coated acicular iron powder were
mixed in a ratio of Nd=28 weight%, B=1 weight% and iron=balance, the mixed powder
was compacted under 2t/cm² pressure in a 5cmx5cmx5cm mold and the molded powder was
heated at 1080°C for 2 hours (heating up rate of 5°C/min) in the presence of a magnetic
field of 15KOe (Oersted) to obtain a sintered magnet. The resulted magnet had the
following magnetic properties:
- iHc:
- 9371 Oe
- Br:
- 13560 Gauss
- BHmax:
- 43.4 MGOe
[Comparative Example 1]
[0021] An acicular iron powder, an Nd powder and an boron powder were prepared in the same
manner as that for Example 1 except for no coating of aluminum phosphate was conducted
to those kinds of powder. A sintered magnet was prepared under the same formulation
of components and condition as those for Example 1 in which no specific precaution
was taken against shutting down of air. The resulted magnet had the following magnetic
properties:
- iHc:
- 8434 Oe
- Br:
- 12204 Gauss
- BHmax:
- 39.0 MGOe
[Example 2]
[0022] To a sintered magnet prepared by the same method as that for Example 1 was added
a 10% ethanol solution containing aluminum phosphate of an amount corresponding to
5 weight% of the magnet, and the ethanol was evaporated. The dried magnet was subjected
to hydrogen occlusion for 1 hour in a rotary kiln under ventilation of 10 liter/min
of 100 vol% hydrogen gas and at 880°C (heating up rate was 5°C/min), and then was
subjected to emission of hydrogen in substantial vacuum during maintaining for 1 hour
at the temperature followed by cooling to 200°C (cooling rate was 5°C/min) to disintegrate
the magnet. Three times repetition of the disintegration step resulted in an aluminum
phosphate coated magnet powder having an average particle size of 8µm. A mixture of
90g of the magnet powder and 10g of an epoxy resin (DAINIPPON INK K.K; for bond magnet)
as a binder was charged in a mold and subjected to a magnetic field of 150Koe, a pressure
of 6t/cm², raising of temperature up to 150°C at 5°C/min rate and heating for 2 hours
at the temperature to obtain a bond magnet. The resulted magnet had the following
magnetic properties:
- iHc:
- 15000 Oe
- Br:
- 11760 Gauss
- BHmax:
- 31.9 MGOe
[Comparative Example 2]
[0023] An acicular iron powder, an Nd powder and an boron powder were prepared by the same
method as those for Example 1 except for no coating of aluminum phosphate was conducted
to those kinds of powder. A sintered magnet was prepared under the same formulation
of component and condition as those for Example 1 in which no specific precaution
was taken against shutting down of air. A magnet powder was prepared from the sintered
magnet in the same manner as that for Example 2 except for no coating of aluminum
phosphate was conducted. A bond magnet was prepared from the magnet powder under the
same condition as those for Example 2 in which no specific precaution was taken against
shutting down of air. The resulted magnet had the following magnetic properties:
- iHc:
- 12000 Oe
- Br:
- 9408 Gauss
- BHmax:
- 25.5 MGOe
[0024] By making comparisons of magnetic properties between Example 1 and Comparative Example
1 for the sintered magnet as well as Example 2 and Comparative Example 2 for the bond
magnet, the effect of the present invention can be understood clearly.
[0025] According to the present invention, it is possible to prepare easily a sintered-
or a bond- rare earth element·iron·boron magnet superior in the magnetic properties
with stable performance.
1. A method of producing sintered rare earth element·iron·boron magnets which comprises
mixing in a scheduled ratio an acicular iron powder coated with a coating material,
a rare earth element powder coated with a coating material and a boron powder coated
with a coating material, and subjecting the mixture to compression molding followed
by sintering of the molded mixture in the presence of a magnetic field.
2. A method of producing sintered rare earth element·iron·boron magnets according to
claim 1, in which the coating material is aluminum phosphate.
3. A method of producing sintered rare earth element·iron·boron magnets according to
claim 1 or 2, in which the mixing ratio between the rare earth element powder, the
boron powder and the acicular iron powder is 20-40 weight% for rare earth element
powder, 0.5-3 weight% for boron powder and the rest for acicular iron powder.
4. A method of producing sintered rare earth element·iron·boron magnets according to
claim 1, 2 or 3, in which the acicular iron powder is one prepared by reducing acicular
FeOOH (geothite) crystal under heating in hydrogen atmosphere, the rare earth element
powder is one prepared by hydrogen-disintegration of rare earth element lumps wherein
hydrogen-occluded rare earth element lumps resulted from heating rare earth element
lumps under hydrogen atmosphere are subjected to hydrogen emission under substantial
vacuum to cause disintegration of the hydrogen-occluded rare earth element lumps,
and the born powder is one prepared by hydrogen-disintegration of boron lumps wherein
hydrogen-occluded boron lumps resulted from heating boron lumps under hydrogen atmosphere
are subjected to hydrogen emission under substantial vacuum to cause disintegration
of the hydrogen-occluded boron lumps.
5. A method of producing sintered rare earth element·iron·boron magnets according to
claim 4, in which the temperature for reducing the acicular iron powder under hydrogen
atmosphere is 300-500°C, the temperature for heating of the rare earth element lumps
or boron lumps under hydrogen atmosphere to occlude hydrogen is 800-900°C, and the
temperature for emitting hydrogen under substantial vacuum from the hydrogen-occluded
rare earth element lumps or boron lumps is not lower than 100°C.
6. A method of producing sintered rare earth element·iron·boron magnets according to
claim 2, 3, 4 or 5, in which the acicular iron powder has a length of not longer than
10µm, the rare earth element powder coated with aluminum phosphate has an average
particle size of 1-10µm, and the boron powder coated with aluminum phosphate has an
average particle size of 1-10µm.
7. A method of producing a sintered rare earth element·iron·boron magnets which comprises
mixing in a scheduled ratio an acicular iron powder coated with aluminum phosphate
prepared by reducing acicular FeOOH (geothite) crystal coated with aluminum phosphate
under heating in hydrogen atmosphere, a rare earth element powder coated with aluminum
phosphate prepared by hydrogen-disintegration of rare earth element lumps coated with
aluminum phosphate wherein hydrogen-occluded coated rare earth element lumps resulted
from heating coated rare earth element lumps under hydrogen atmosphere are subjected
to hydrogen emission under substantial vacuum to cause disintegration of the hydrogen-occluded
coated rare earth element lumps, and a boron powder coated with aluminum phosphate
prepared by hydrogen-disintegration of boron lumps coated with aluminum phosphate
wherein hydrogen-occluded coated boron lumps resulted from heating coated boron lumps
under hydrogen atmosphere are subjected to hydrogen emission under substantial vacuum
to cause disintegration of the hydrogen-occluded coated boron lumps, and subjecting
the mixture to compression molding followed by sintering of the molded mixture in
the presence of a magnetic field.
8. A method of producing sintered rare earth element·iron·boron magnets according to
claim 7, in which the mixing ratio between the rare earth element powder, the boron
powder and the acicular iron powder is 20-40 weight% for rare earth element powder,
0.5-3 weight% for boron powder and the rest for acicular iron powder.
9. A method of producing sintered rare earth element·iron·boron magnets according to
claim 7 or 8, in which the temperature for reducing the acicular iron powder under
hydrogen atmosphere is 300-500°C, the temperature for heating the rare earth element
lumps or boron lumps under hydrogen atmosphere to occlude hydrogen is 800-900°C, and
the temperature for emitting hydrogen under substantial vacuum from the hydrogen-occluded
rare earth element lumps or boron lumps is not lower than 100°C.
10. A method of producing sintered rare earth element·iron·boron magnets according to
claim 7, 8 or 9, in which the acicular iron powder coated with aluminum phosphate
has a length of not longer than 10µm, the rare earth element powder coated with aluminum
phosphate has an average particle size of 1-10µm, and the boron powder coated with
aluminum phosphate has an average particle size of 1-10µm.
11. A method of producing bond rare earth element·iron·boron magnets which comprises mixing
in a scheduled ratio an acicular iron powder coated with a coating material, a rare
earth element powder coated with a coating material, and a boron powder coated with
a coating material, preparing from the mixture a sintered magnet by compression-molding
and sintering in the presence of a magnetic field, preparing a magnet powder by hydrogen-disintegration
of the magnet wherein a hydrogen-occluded magnet resulted from heating the magnet
under hydrogen atmosphere is subjected to hydrogen emission under substantial vacuum
to cause disintegration of the hydrogen-occluded magnet, coating the magnet powder
with a coating material, mixing the coated magnet powder with a binder, and compression
molding the mixture under heating in the presence of a magnetic field.
12. A method of producing bond rare earth element·iron·boron magnets according to claim
11, in which the coating material is aluminum phosphate.
13. A method of producing bond rare earth element·iron·boron magnets according to claim
11 or 12, in which the mixing ratio between the rare earth element powder, the boron
powder and the acicular iron powder is 20-40 weight% for rare earth element powder,
0.5-3 weight% for boron powder and the rest for acicular iron powder.
14. A method of producing bond rare earth element·iron·boron magnets according to claim
11, 12 or 13, in which the acicular iron powder is one prepared by reducing acicular
FeOOH (geothite) crystal under heating in hydrogen atmosphere, the rare earth element
powder is one prepared by hydrogen-disintegration of rare earth element lumps wherein
hydrogen-occluded rare earth element lumps resulted from heating rare earth element
lumps under hydrogen atmosphere are subjected to hydrogen emission under substantial
vacuum to cause disintegration of the hydrogen-occluded rare earth element lumps,
and the born powder is one prepared by hydrogen-disintegration of boron lumps wherein
hydrogen-occluded boron lumps resulted from heating boron lumps under hydrogen atmosphere
are subjected to hydrogen emission under substantial vacuum to cause disintegration
of the hydrogen-occluded boron lumps.
15. A method of producing bond rare earth element·iron·boron magnets according to claim
14, in which the temperature for reducing the acicular iron powder under hydrogen
atmosphere is 300-500°C, the temperature for heating the rare earth element lumps
or boron lumps under hydrogen atmosphere to occlude hydrogen is 800-900°C, and the
temperature for emitting hydrogen under substantial vacuum from the hydrogen-occluded
rare earth element lumps or boron lumps is not lower than 100°C.
16. A method of producing bond rare earth element·iron·boron magnets according to claim
12, 13, 14 or 15, in which the acicular iron powder coated with aluminum phosphate
has a length of not longer than 10µm, the rare earth element powder coated with aluminum
phosphate has an average particle size of 1-10µm, and the boron powder coated with
aluminum phosphate has an average particle size of 1-10µm.
17. A method of producing bond rare earth element·iron·boron magnets according to claim
11, 12, 13, 14, 15 or 16, in which the binder is a vitrification agent or an epoxy
resin.
18. A method of producing bond rare earth element·iron·boron magnets which comprises mixing
in a scheduled ratio an acicular iron powder coated with aluminium phosphate prepared
by reducing acicular FeOOH (geothite) crystal coated with aluminum phosphate under
heating in hydrogen atmosphere, a rare earth element powder coated with aluminum phosphate
prepared by hydrogen-disintegration of rare earth element lumps coated with aluminum
phosphate wherein hydrogen-occluded rare earth element lumps resulted from heating
rare earth element lumps under hydrogen atmosphere are subjected to hydrogen emission
under substantial vacuum to cause disintegration of the hydrogen-occluded rare earth
element lumps, and a born powder coated with aluminum phosphate prepared by hydrogen-disintegration
of boron lumps coated with aluminum phosphate wherein hydrogen-occluded boron lumps
resulted from heating boron lumps under hydrogen atmosphere are subjected to hydrogen
emission under substantial vacuum to cause disintegration of the hydrogen-occluded
boron lumps, preparing from the mixture a sintered magnet by compression-molding and
sintering in the presence of a magnetic field, coating the sintered magnet with aluminum
phosphate, preparing a magnet powder by hydrogen-disintegration of the aluminum phosphate
coated magnet wherein a hydrogen-occluded magnet resulted from heating the magnet
under hydrogen atmosphere is subjected to hydrogen emission under substantial vacuum
to cause disintegration of the hydrogen-occluded magnet, mixing the magnet powder
with a binder, and compression molding the mixture under heating and in the presence
of a magnetic field.
19. A method of producing bond rare earth element·iron·boron magnets according to claim
18, in which the mixing ratio between the rare earth element powder, the boron powder
and the acicular iron powder is 20-40 weight% for rare earth element powder, 0.5-3
weight% for boron powder and the rest for acicular iron powder.
20. A method of producing bond rare earth element·iron·boron magnets according to claim
18 or 19, in which the temperature for reducing the acicular iron powder under hydrogen
atmosphere is 300-500°C; the temperature for heating the rare earth element lumps
or boron lumps under hydrogen atmosphere to occlude hydrogen is 800-900°C; and the
temperature for emitting hydrogen under substantial vacuum from the hydrogen-occluded
rare earth element lumps or boron lumps is not lower than 100°C.
21. A method of producing bond rare earth element·iron·boron magnets according to claim
18, 19 or 20, in which the acicular iron powder coated with aluminum phosphate has
a length of not longer than 10µm, the rare earth element powder coated with aluminum
phosphate has an average particle size of 1-10µm, and the boron powder coated with
aluminum phosphate has an average particle size of 1-10µm.
22. A method of producing bond rare earth element·iron·boron magnets according to claim
18, 19, 20 or 21, in which the binder is a vitrification agent or an epoxy resin.